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Central coast designs: The Eightball Express. Taking off with convention, cruising with improvements and landing with absolute successThe airline industry is very competitive, resulting in most U.S. and many international airlines being unprofitable. Because of this competition the airlines have been engaging in fare wars (which reduce revenue generated by transporting passengers) while inflation has increased. This situation of course is not developing revenue for the airlines. To revive the airlines to profitability, the difference between revenue received and airline operational cost must be improved. To solve these extreme conditions, the Eightball Express was designed with the main philosophy of developing an aircraft with a low direct operating cost and acquisition cost. Central Coast Designs' (CCD) aircraft utilizes primarily aluminum in the structure to minimize manufacturing cost, supercritical airfoil sections to minimize drag, and fuel efficient engines to minimize fuel burn. Furthermore, the aircraft was designed using Total Quality Management and Integrated Product Development to minimize development and manufacturing costs. Using these primary cost reduction techniques, the Eightball Express was designed to meet the Lockheed/AIAA Request for Proposal (RFP) requirements of a low cost, 153 passenger, 3000 nm. range transport. The Eightball Express is able to takeoff on less than a 7000 ft. runway, cruise at Mach 0.82 at an altitude of 36,000 ft. for a range of 3,000 nm., and lands on a 5,000 ft. runway. lt is able to perform this mission at a direct operating cost of 3.51 cents/available seat mile in 1992 dollars while the acquisition cost is only $28 million in 1992 dollars. By utilizing and improving on proven technologies, CCD has produced an efficient low cost commercial transport for the future.
Document ID
19950006230
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Davis, Ryan Edwin
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Dawson, Anne Marie
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Fecht, Paul Hans
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Fry, Roman Zyabash
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Vantriet, Robert
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Macabantad, Dominique Dujale
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Miller, Robert Glenn
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Perez, Gustavo, Jr.
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Weise, Timothy Michael
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-197181
NAS 1.26:197181
Report Number: NASA-CR-197181
Report Number: NAS 1.26:197181
Accession Number
95N12643
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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